Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Pressure sensitive paint measurement in a hypersonic shock tunnel


    Contributors:

    Conference:

    21st Aerodynamic Measurement Technology and Ground Testing Conference ; 2000 ; Denver , CO , U.S.A.



    Publication date :

    2000-01-01



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




    Global Heat Transfer Measurement in a Hypersonic Shock Tunnel Using Temperature-Sensitive Paint

    Nakakita, Kazuyuki / Osafune, Tatsuya / Asai, Keisuke | AIAA | 2003


    Global Heat Transfer Measurement in a Hypersonic Shock Tunnel Using Temperature-Sensitive Paint

    Nakakita, K. / Osafune, T. / Asai, K. et al. | British Library Conference Proceedings | 2003



    Pressure sensitive paint application in shock wind tunnel

    Borovoy, V. / Bykov, A. / Mosharov, V. et al. | IEEE | 1995


    Pressure Sensitive Paint Application in Shock Wind Tunnel

    Borovoy, V. / Bykov, A. / Mosharov, V. et al. | British Library Conference Proceedings | 1995